Test techniques to determine Fasthawk missile aerodynamics including inlet effects-Reference-Cited by-同舟云学术

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Test techniques to determine Fasthawk missile aerodynamics including inlet effects

Published:1999-01-11 Issue: Volume: Page:
ISSN:
Container-title:37th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Bowcutt Kevin¹,Burrows Richard¹,Weir Jeffery¹

Affiliation:

1. Boeing Co., Long Beach, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-432

Reference6 articles.

1. Hughes, M. Terrance, "Results of Testing a Boeing North American 0.1g-Scale Fasthawk Missile Model in the Micro Craft 7 by 7 Foot Trisonic Wind Tunnel (TWT 644).", Micro Craft Report number MC98002, dated January 14,1998.

2. Hughes, M. Terrance, "Results of Testing a Boeing North American 0.1g-Scale Fasthawk Missile Model in the NTS 4-ft High Speed Wind Tunnel", Micro Craft Report Number MC98003, dated January 28,1998.

3. Wardlaw, A.B.; Priolo, F.J.Applying the Zeus Code", NSWC TR 86-508,31 December 1986.

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